Clip with fuild dynamic shape

ABSTRACT

A clip for attachment as an edge. The clip having two symmetric sides, each side composed of five arcs. A first arc of the side starting at the midpoint of the nose having a radius of 0.2476 inches and an arc length of 0.22395 inches. A second arc connected to the first arc having a radius of 0.5832 inches and an arc length of 0.0947 inches. A third arc connected to the second arc having a radius of 0.4636 inches and an arc length of 0.1682 inches. A fourth arc connected to the third arc having a radius of 0.3822 inches and an arc length of 0.2263 inches. A fifth arc connected to the fourth arc having an arc having a radius of 0.3291 inches and an arc length of 0.1917 inches. The fifth arc of each side forming the slot end on the clip.

This application claims the benefit of and incorporates by referenceU.S. Provisional Application No. 61/820,887 filed May 8, 2013 and U.S.Provisional Application No. 61/916,357 filed Dec. 16, 2013.

BACKGROUND

The present invention generally relates to shapes used in fluid flow.More specifically, the present invention relates surface shapes andfluid flow over those shapes.

There are many shapes on the market to enhance fluid flow. Not much workhas been done to simply add a device to a shape to enhance fluid flowover that shape. What would be useful is a shape that could be used as aleading edge or trailing edge to attach to a shape to enhance fluid flowover that shape.

It is an object of the present invention to provide a clip to add aleading edge or trailing edge to a shape to enhance fluid flow over thatshape.

SUMMARY OF THE INVENTION

A clip for attachment as an edge. The clip having two symmetric sides,each side composed of five arcs. A first arc of the side starting at themidpoint of the nose having a radius of 0.2476 inches and an arc lengthof 0.22395 inches. A second arc connected to the first arc having aradius of 0.5832 inches and an arc length of 0.0947 inches. A third arcconnected to the second arc having a radius of 0.4636 inches and an arclength of 0.1682 inches. A fourth arc connected to the third arc havinga radius of 0.3822 inches and an arc length of 0.2263 inches. A fiftharc connected to the fourth arc having an arc having a radius of 0.3291inches and an arc length of 0.1917 inches. The fifth arc of each sideforming the slot end on the clip.

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 is a perspective view of a wind turbine according to the presentinvention.

FIG. 2 is an exploded view of a wind turbine according to the presentinvention.

FIG. 3 is an exploded view of a wind turbine according to the presentinvention.

FIG. 4 is an end view of a vane according to the present invention.

FIG. 5 is a perspective view of a vane according to the presentinvention.

FIG. 6 is an end view of a turbine blade according to the presentinvention.

FIG. 7 is a perspective view of a turbine blade according to the presentinvention.

FIG. 8 is a top view of a wind turbine according to the presentinvention.

FIG. 9 is a profile view of a clip according to the present invention.

FIG. 10 is a segment view of a clip according to the present invention.

FIG. 11 is a top view of a flat blade assembly with clip according tothe present invention.

FIG. 12 is a perspective view of a frame assembly according to thepresent invention.

FIG. 13 is an exploded view of a frame assembly according to the presentinvention.

FIG. 14 is a perspective view of a turbine assembly in a frame assemblyaccording to the present invention.

FIG. 15 is a schematic view of a vane position according to the presentinvention.

FIG. 16 is a schematic view of a blade position according to the presentinvention.

FIG. 17 is a perspective view of a wind flow about a wind turbineaccording to the present invention.

FIG. 18 is a top view of a wind flow about a wind turbine according tothe present invention.

FIG. 19 is a perspective view of a two flat blade assembly according tothe present invention.

FIG. 20 is a perspective view of a Savonius scoop blade assemblyaccording to the present invention.

FIG. 21 is a perspective view of a three curved blade assembly accordingto the present invention.

FIG. 22 is a perspective view of a two flat blade assembly without clipaccording to the present invention.

FIG. 23 is a perspective view of a two flat blade assembly with clipaccording to the present invention.

DETAILED DESCRIPTION

The present invention is a wind turbine used to convert wind intorotational energy. FIGS. 1-8 show a first embodiment. FIG. 1 shows aperspective top and side view of the wind turbine 10 of the firstembodiment. FIG. 2 shows a side exploded view and FIG. 3 shows aperspective exploded view of the wind turbine 10. FIGS. 1-3 show a frameassembly 12 and with a turbine assembly 14 within the frame assembly 12.

The frame assembly 12 is a stationary circular frame that has a multipleof airfoil shaped vanes 16 that take advantage of the Coand{hacek over(a)} effect, Bernoulli's principle, viscous shear and a resultingcreation of a low pressure area. The vanes 16 are vertically mounted andattached to the outer perimeter of frame assembly 12 at an angle. Thevanes 16 include a round outer edge with a curved dip just in front ofthe curved outer semi-circle, to aid in using the Coand{hacek over (a)}effect, Bernoulli's principle, viscous shear and the resulting creationof a low pressure area. In the center of the frame assembly 12, is thecircular turbine assembly 14 that rotates within the frame assembly 12.The turbine assembly 14 includes multiple angled airfoil shaped turbineblades 18 with a specific shape to compress and accelerate the air anddirect the air to opposite turbine blades 18 in order to create lift andtorque a second time within the turbine assembly 14 before the air exitswind turbine 10 during rotation. The turbine blades 18 can be angled atdifferent angles depending on the number of turbine blades 18, butideally around 22.5 degrees is the best angle. The air entering into theturbine assembly 14 from the frame assembly 12 passes a turbine blade 18by moving over the curved surface of the turbine blade 18 creating a lowpressure area in front of the turbine blade 18 and creating lift that isimparted to the forward momentum of the turbine blade 18 to createrotation of the turbine assembly 14. The turbine assembly 14 can beconnected to a load shaft 20 that spins a load such as a generator.

The frame assembly 12 includes vanes 16, a bottom vane retainer 22 and atop vane retainer 24, as shown in FIGS. 2-3. The vanes 16 include abottom vane end 26, a top vane end 28. The vanes 16 include anaerodynamic shape vane between the bottom vane end 26 and the top vaneend 28. The bottom vane retainer 22 and top vane retainer 24 includevane tabs 30 and weight reduction holes 32. The bottom vane retainer 22and top vane retainer 24 each have an area about the perimeter thatforms a mounting ring 35 from mounting of the vanes 16. FIG. 3 shows apair of vane tabs 30 on the ring 35 of the bottom vane retainer 22 foreach vane 16. Each pair of vane tabs 30 on the bottom vane retainer 22are shaped to receive the bottom vane end 26 of the vane 16 between thepair of vane tabs 30. The bottom vane end 26 is secured between the pairof vane tabs 30 and hence the bottom vane retainer 22. The top vaneretainer 24 is the same as the bottom vane retainer 22 as shown in FIG.2, where the paired vane tabs 30 of top vane retainer 24 face the pairedvane tabs 30 of the bottom vane retainer 22. The top vane end 28 of thevane 16 is secured between a pair of vane tabs 30 of the top vaneretainer 24 in the same manner as the vane 16 is secured to the bottomvane retainer 22. A plurality of vanes 16 are secured between the topvane retainer 24 and the bottom vane retainer 22 to form the frameassembly 12.

The turbine assembly 14 includes turbine blades 18, a bottom bladeretainer 34 and a top blade retainer 36, as shown in FIGS. 2-3. Theturbine blades 18 include a bottom blade end 38, a top blade end 40. Theturbine blades 18 include a shaped blade between the bottom blade end 38and the top blade end 40. The bottom blade retainer 34 and top bladeretainer 36 include blade tabs 42 and weight reduction holes 32. Thebottom blade retainer 34 and top blade retainer 36 each have an areaabout the perimeter that forms a mounting ring 44 from mounting of theturbine blades 18. FIG. 3 shows a pair of blade tabs 42 on the bottomblade retainer 34 for each turbine blade 18. Each pair of blade tabs 42on the bottom blade retainer 34 are shaped to receive the bottom bladeend 38 of the turbine blade 18 between the pair of blade tabs 42. Thebottom blade end 38 is secured between the pair of blade tabs 42 andhence the bottom blade retainer 34. The top blade retainer 36 is thesame as the bottom blade retainer 34 as shown in FIG. 2, where thepaired blade tabs 42 of top blade retainer 36 face the paired blade tabs42 of the bottom blade retainer 34. The top blade end 40 of the turbineblade 18 is secured between a pair of blade tabs 42 of the top bladeretainer 36 in the same manner as the turbine blade 18 is secured to thebottom blade retainer 34. A plurality of turbine blades 18 are securedbetween the top blade retainer 36 and the bottom blade retainer 34 toform the turbine assembly 14. The top vane retainer 24, bottom vaneretainer 22, top blade retainer 36 and bottom blade retainer 34 eachhave a shaft hole 46. FIG. 2 shows a load shaft 48 that mounts in theshaft holes 46. The load shaft 48 is securely attached at the shaftholes 46 of top blade retainer 36 and bottom blade retainer 34 ofturbine assembly 14, such that rotation of the turbine assembly 14rotates the load shaft 48. Shaft bearings 50 are shown that attach tothe top vane retainer 24 and bottom vane retainer 22 of the frameassembly 12. The shaft bearings 50 receive the load shaft 48 and allowthe load shaft 48 to rotate without the frame assembly 12 rotating.

FIG. 4 shows the profile of the vane 16. FIG. 5 shows a threedimensional view of the vane 16. The profile includes a half circleleading edge 52, where the radius of the half circle leading edge 52depends on the size of the vane 16. Extending from each end 54 of thehalf circle leading edge 52 are sides 56 of the vane 16 that cometogether to form a trailing edge 58. The sides 56 are shown curvinginward from ends 54 of the half circle leading edge 52 before making astraight run to form the trailing edge 58. The sides 56 could alsoextend in a straight line from the ends 54 of the half circle leadingedge 52 to form the trailing edge 58. FIG. 6 shows the profile of theturbine blade 18. FIG. 7 shows a three dimensional view of the turbineblade 18. The profile includes a half circle leading edge 60, where theradius of the half circle leading edge 60 depends on the size of theturbine blade 18. The profile includes a half circle trailing edge 62,where the radius of the half circle trailing edge 62 depends on the sizeof the turbine blade 18. Extending from each end 54 of the leading edge60 and the trailing edge 62 are a top side 64 and a bottom side 66 ofthe turbine blade 18. The top side 64 is shown curving outward towardsthe middle of the top side 64 between the leading edge and the trailingedge. The bottom side 66 is shown curving inward towards the middle ofthe bottom side 66 between the leading edge 60 and the trailing edge 62of the turbine blade 18. The top side 64 and the bottom side 66 form anaerodynamic shape between the leading edge 60 and the trailing edge 62of the turbine blade 18. The top side 64 and the bottom side 66 couldalso extend in a straight line between the leading edge 60 and thetrailing edge 62 of the turbine blade 18.

FIG. 8 shows the airflow of the wind through the frame assembly 12 andthe turbine assembly 14. For discussion purposes, the top vane retainer24 is removed from the frame assembly 12. FIG. 8 depicts what isbelieved to happen to airflow of wind as it hits the wind turbine 10 ofFIGS. 1-7 from any given direction. It is believed that Coand{hacek over(a)} effect and Bernoulli's principle pertaining to the acceleration ofair are part of what causes the airflow depicted in FIG. 8. FIG. 8 showsthe wind turbine 10 in wind coming from direction A. The frame assembly12 is a stationary circular frame with the fixed vertically mountedvanes 16 arranged around the outer perimeter of the frame assembly 12.The vanes 16 are angled in the frame assembly 12 between 25-40 degrees,depending on diameter of frame assembly 12. Purpose of the frameassembly 12 is to cause the wind coming from any direction to bedirected to force forward motion of turbine blades 18 in the directionof rotation of the turbine assembly 14. The frame assembly 12 capturesair greater than the width of the frame assembly 12, as shown in FIG. 8.FIG. 8 shows capturing wind along the sides of the frame assembly 12 atpoints B and D. This happens because the air that is blowing outside theframe assembly 12 is literally sucked in between the vanes 16 on thesides and backside of the frame assembly 12. The acceleration of airtowards the vanes 16 in the frame assembly 12 cut through air on thereturn side B of the circular path. The air flow on side B is convertedfrom being a point of drag on the rotation of the rotating turbineblades 18 of the turbine assembly 14 to a positive force of momentumthat aides in creating rotation of the turbine assembly 14 instead ofdrag by the use of the above listed principals. The singular directionalair flow at sections B, A, and D all combine to add to the speed ofrotation of the turbine assembly 14. This happens because the air thatis blowing outside the frame assembly 12 is flowing in the oppositedirection of the turbine blades 18 rotation and travels around the outerperimeter and is then sucked in between the vanes 16 nearest to thereturn path (junction of C and D) of the forward moving air due to thelow pressure area created by accelerating air. This is due to areas ofhigh pressure and low pressure being created by the turbine blades 18.The angle and the placement in the vanes 16 in the frame assembly 12does not allow for the wind to have a direct negative impact on theturbine blades 18 of the turbine assembly 14 since all air entering isin the direction of the forward rotation of the turbine assembly 14.

The acceleration and change of direction of existing wind to operate thewind turbine 10 is achieved with this design. The wind is redirectedtoward the forward motion of the turbine assembly 14 with the use of aspecial aerodynamic shape leading edge creating a positive force inplace of the drag created by turbine blades 18 of the turbine assembly14 spinning into the direction of the wind. The use of this specialaerodynamic shape of the half circle leading edge allows for smooth flowof air into and out of the wind turbine 10. As described above, the airflow on the left side of FIG. 8 is converted from a point of drag on therotation to a positive force of momentum creating rotation instead ofdrag by the use of the above principals. The entire width and height ofthe air flow from the wind all combine to add to the forward rotation ofthe turbine assembly 14. The purpose of the frame assembly 12 is tocause the wind coming from any direction to be directed toward forwardmotion of turbine blades 18 and eliminate drag and creating a positiveforce in its place using the Coand{hacek over (a)} effect, Bernoulli'sprinciple, viscous shear and the resulting creation of a low pressurearea. The frame assembly 12 captures air greater than the width ofitself using viscous shear. This happens because the air of the windthat is blowing outside the frame assembly 12 is redirected toward therotation of the turbine blades 18 inside frame assembly 12 and thepulling adjacent air along that would not normally enter prior verticalwind turbine designs. The angle and the placement of the vanes 16 in theframe assembly 12 does not allow for the wind to have a direct negativeimpact on the spinning turbine blades 18 but instead creates a positiveforce in place of the drag, since all air entering is in the directionof rotation of the turbine blades 18. It is believed that a prime numberof turbine blades 18 is the most effective configuration of turbineblades 18 in the turbine assembly 14.

For a second embodiment, a clip of a special fluid dynamic shape wasdeveloped to replace the semi-circle leading edges and trailing edges ofthe first embodiment. The clip is shown in FIG. 9 and has proven to beuseful as a leading edge and trailing edge for many devices that employfluid dynamics. In experiments, the clip was used as an aerodynamic edgeon aerodynamic shapes such as airfoils. In the experiments, the clip hasproven to increase lift on the shape at lower air velocities, but theclip can also be used to improve any fluid flow over a shape. The clipcan be added to a blade that has a flat bar shape to almost any shapedblade that employs techniques to enhance fluid flow over a shape. FIG. 9shows the dimensions of the outside surface of a clip for use with awind turbine having a frame assembly diameter in the range of 12 inchesto 48 inches and turbine assembly diameter in the range of 8 inches to36 inches. The clip is symmetric about a line through points A and B andis shown to be made up of five arcs. FIG. 10 shows an enlarged viewbetween points D and G. Between points A and G, is an arc having aradius of 0.2476 inches and an arc length of 0.23895. Between points Gand F, is an arc having a radius of 0.5832 inches and an arc length of0.0948 inches. Between points F and E, is an arc having a radius of0.4636 inches and an arc length of 0.1691 inches. Between points E andD, is an arc having a radius of 0.3822 inches and an arc length of0.2298 inches. Between points D and C, is an arc having a radius of0.3291 inches and an arc length of 0.1945 inches. FIG. 9 also showsdistance between points from a datum at point A and distance betweenpoints G with A as the midpoint. FIG. 10 shows the distance betweenpoints G, F, E and D. The arc between G and A for both sides forms anose end. The outside surface of the clip can be enlarged or reduced insize by scaling the size of the arc radius and arc length of each arcbetween the points by applying the same percentage of change to eacharc.

The opening at the blade end 67 of the clip between points C in FIG. 9is for receiving a blade or other fluid dynamic shape. FIG. 11 shows aflat blade assembly 68 of two clips 70 on each end of a flat blade 72.The flat blade includes side 74, side 76 and thickness 78. A blade usedwith the clip can be of any thickness, but there is a requirement thatpoint C of FIG. 9 connects to the sides of the blade in a way such thatthere is no opening between points C and the sides of the blade. Thisrequirement is for keeping the flow off of the clip separated from otherairflow, which causes the air to be drawn around the one side more thanthe other of the clip and hence the flat blade assembly 68. Thisrequirement is not only subject to flat blades, but all blade profilesthat incorporate the use of the clip. Therefore, the distance betweenpoints C of the clip will vary depending on the thickness of the flatblade. If it is desired to use a blade of a thickness that is less thanthe opening of the blade end 67 of any particular sized clip, a gapfiller can be used between points C and the sides of the blade. Anexample of a gap filler is a straight wall of material between points Cand the sides of the blade. The clip can be applied to many applicationsthat involve fluid dynamics, where the second embodiment will be oneexample of the application of the clip. Each clip includes a bladechannel 80 inside the clip to hold the blade 72 and clip 70 in positiontogether, as shown in FIG. 11. FIG. 11 shows the behavior of fluid flowfrom the wind, where the air directed at almost 90 degrees from the nose82 of the clip 70 at point 84 versus wind that has direct impingement onthe nose 82. The air flow from the wind is directed about side 86 andnose 82 of the clip 70 and then flows about the other side 88 of theclip 70. The airflow then follows side 74 of the flat blade 72 towardsthe other clip 70 for exiting pass the flat blade assembly 68. Theunique feature of the flat blade assembly 68 using the clip 70 is howthe air is captured in the area about the side 86 and nose 82 of theclip 70 and then forced along the flat blade assembly 68.

FIGS. 12-13 shows a frame assembly 90 of the second embodiment with atop vane retainer 92, bottom vane retainer 94 and using the flat bladeassembly 68 of FIG. 11 for the vanes 96. FIG. 14 shows a turbineassembly 98 within the frame assembly 90 of FIGS. 12-13. The turbineassembly 98 is shown with a top blade retainer 100, bottom bladeretainer 102 and using the flat blade assembly 68 of FIG. 11 for theturbine blades 104. FIGS. 13-14 also show a load shaft 106 forconnecting to a load. FIG. 14 shows shaft mounts 108 attached to the topblade retainer 100 and bottom blade retainer 102 to secure the loadshaft 106 so that the load shaft 106 rotates with the turbine assembly98 during turbine assembly 98 rotation. FIG. 14 shows a shaft bearing110 which mounts to the outside surface of the top vane retainer 92 toreceive the load shaft 106. The outside surface of the bottom vaneretainer 94 would also have a shaft bearing 110, but is not shown. Thetop vane retainer 92, bottom vane retainer 94, top blade retainer 100and bottom blade retainer 102 all have a shaft hole 112 similar to thefirst embodiment to allow passage of the load shaft 106. The shaftbearings 110 allow the load shaft 106 to rotate within the frameassembly 90, as the frame assembly 90 is stationary. The vanes 96 andturbine blades 104 can be mounted in various ways, including using themodern technology of printing the frame assembly 90 and turbine assembly98 each as one piece with a 3-D printing device.

FIG. 15 shows how to define positioning of the vanes which can beapplied to both embodiments. FIG. 15 shows an imagery line drawn 114from the center of the frame assembly to the leading edge clip 116 ofthe flat blade assembly 118 used for the vanes. An angle of 45 degreesis formed between the flat blade assembly 118 and the imagery line 114due to the position of the trailing edge clip 120 of the flat bladeassembly 118. A counter clockwise rotation of the trailing edge clip 120from the imagery line 114 is considered positive angle and a clockwiserotation (not shown) from the imagery line 114 is considered a negativeangle. A flat blade assembly position of a vane that has a positiveangle produces the turbine assembly rotation in the clockwise directionand a position of a vane that has a negative angle produces the turbineassembly rotation in the counter clockwise direction. A flat bladeassembly position for the vanes of 35 to 50 degrees of angle in thepositive or negative direction works well and an angle of +/−45 degreesappears to be optimal in limited testing. FIG. 16 shows how to definepositioning of the turbine blades. FIG. 16 shows an imagery line 122drawn from the center of the turbine assembly to the leading edge clip124 of the flat blade assembly 126 used for the turbine blades. Apositive angle of 25 degrees formed between the flat blade assembly 126and the imagery line 122 due to the position of the trailing edge clip128 of the flat blade assembly 126 used as a turbine blade is shown inFIG. 16. A counter clockwise rotation of the trailing edge clip 128 fromthe imagery line 122 is considered positive angle and a clockwiserotation is considered a negative angle. FIG. 16, also shows a negativeangle of 10 degrees formed between the flat blade assembly 126 and theimagery line 122 due to the position of the trailing edge clip 128 ofthe flat blade assembly 126 used as a turbine blade. A flat bladeassembly position for the turbine blades of −20 degrees to +25 degreesof angle works well. An angle of −10 degrees appears to be optimal inlimited testing. The angles show are for a turbine assembly that rotatesin the clockwise direction. The angles would be reversed for a turbineassembly designed to rotate in the counter clockwise direction, where+20 degrees to −25 degrees of angle would work well and +10 degrees ofangle would be optimal.

FIGS. 17-18 show airflow from a wind direction W flowing about andthrough the wind turbine of the second embodiment. For the wind turbineof FIGS. 17-18, the turbine assembly 98 rotates in a clockwise directionwhen viewed from the top vane retainer 92. The clockwise rotation is duethe positioning of the vanes 96 in the frame assembly 90, as describedfor FIGS. 15-16. FIGS. 17-18 show the collection of wind thru the frameassembly 90 from not only direct impingement from the wind at point W,but collection of wind on the sides of the frame assembly 90 by the windturbine for used to turn the turbine blades 104. The capture and use ofthe wind in the second embodiment is the same theory as described abovein FIG. 8 for the first embodiment.

Tests were performed on a wind turbine of the second embodiment. Thewind turbine had a frame assembly with a 48 inch diameter and a heightof 28 inches. The vanes were 5 inches wide and there were 20 vanes onthe frame assembly. The turbine assembly had a 36 inch diameter and 13turbine blades that were 8 inches wide. Measured at the shaft was aproduction of 21 lb ft of torque at 91 rpm for a 6.5 m/s wind speed.This model was designed to produce a high torque for a low rpmgenerator. It was found that a reduction in vanes in the frame assemblywill increase rpm but lower torque at the load shaft for the same sizeframe assembly and turbine assembly and an increase in vanes has theopposite effect on torque and rpm at the shaft. Using scale models 6inches high and a 12 inch frame assembly diameter the following resultswere achieved. Testing was done with a two flat blade assembly 130 thatwas 5.5 inches wide and 6 inches high and affixed to a center shaftstraight across from each other, as shown in FIG. 19. A wind speed was10 mph was used and there was no movement attained. The next test withthe same blade assembly 130 was to place them inside the frame assemblyof second embodiment and use the same 10 mph wind, where the blades spun430 rpm. This shows the positive effect of the frame assembly to turnthe air flow and create a one way flow of air inside the frame assemblyand eliminate the drag on the blade spinning into the direction of thewind. A second test was done the same way using a Savonius two scoopdesign blade assembly 132 with 5.5 inch diameter and 6 inches high shownin FIG. 20 without the frame assembly, where the blade assembly 132achieved 392 rpm in the 10 mph wind. When the blade assembly 132 wasplaced inside the frame assembly, the blade assembly 132 achieved 507rpm in the 10 mph wind. FIG. 21 shows a three curved blade assembly 134of 5.5 inches in diameter and 6 inches high. Without the frame assembly,the blade assembly 134 achieved 128 rpm in the 10 mph wind. When theblade assembly 134 was placed inside the frame assembly, a 328 rpm wasachieved in the 10 mph wind. These tests show that the frame assemblywith the design of the clip enhances the rotation of blades inside theframe assembly by the collection of more wind about the frame assemblyversus only allowing direct impingement of the wind on such bladedesigns. FIG. 22 shows a two flat blade assembly 136, which includes twoflat blades 138 and a spindle 140. The flat blade assembly 136 was 5.5inches in diameter and 6 inches high. When a 10 mph wind speed wasapplied, there was no movement caused by the simulated wind. FIG. 23shows the clip 142 in scale added to each flat blade 138 of FIG. 22.When a 10 mph wind speed was applied, the spindle 140 rotated at 370rpm. This shows that the addition of the clip 142 can cause rotation andlift due the aerodynamic shape of the clip 142.

While different embodiments of the invention have been described indetail herein, it will be appreciated by those skilled in the art thatvarious modifications and alternatives to the embodiments could bedeveloped in light of the overall teachings of the disclosure.Accordingly, the particular arrangements are illustrative only and arenot limiting as to the scope of the invention that is to be given thefull breadth of any and all equivalents thereof.

I claim:
 1. A clip for attachment to a structure comprising, an outsidesurface, said clip having a nose end and a slot end, said slot endincluding a slot adapted to receive the structure to be attached to saidclip, said clip having two sides between said nose end and said slotend, each of said two sides starting a midpoint of said nose end andleading towards said slot end, said sides forming said outside surfaceof said clip, each of said sides being composed of five arcs, said fivearcs comprising a first arc of each of said side starting at saidmidpoint of said nose end having a radius of 0.2476 inches and an arclength of 0.22395 inches, a second arc of each of said sides connectedto said first arcs having a radius of 0.5832 inches and an arc length of0.0947 inches, a third arc of each of said sides connected to saidsecond arcs having a radius of 0.4636 inches and an arc length of 0.1682inches, a fourth arc of each of said sides connected to said third arcshaving a radius of 0.3822 inches and an arc length of 0.2263 inches, afifth arc of each of said sides connected to said fourth arcs having anarc having a radius of 0.3291 inches and an arc length of 0.1917 inches,said of each of said fifth arcs of each side forming said slot end andsaid slot.
 2. The clip of claim 1, wherein there is no gap between saidfifth arcs and the structure to be attached to said clip.
 3. A clip forattachment to a structure comprising, an outside surface, said cliphaving a nose end and a slot end, said slot end including a slot adaptedto receive the structure to be attached to said clip, said clip havingtwo sides between said nose end and said slot end, each of said twosides starting a midpoint of said nose end and leading towards said slotend, said sides forming said outside surface of said clip, each of saidsides being composed of five arcs, said five arcs comprising a first arcof each of said side starting at said midpoint of said nose end having aradius of 0.2476 inches and an arc length of 0.22395 inches, a secondarc of each of said sides connected to said first arcs having a radiusof 0.5832 inches and an arc length of 0.0947 inches, a third arc of eachof said sides connected to said second arcs having a radius of 0.4636inches and an arc length of 0.1682 inches, a fourth arc of each of saidsides connected to said third arcs having a radius of 0.3822 inches andan arc length of 0.2263 inches, a fifth arc of each of said sidesconnected to said fourth arcs having an arc having a radius of 0.3291inches and an arc length of 0.1917 inches, said of each of said fiftharcs of each side forming said slot end and said slot, wherein said clipis scaled to be a proper size to mount on a particular sized structureto be attached to said clip by changing arc lengths and arc radius ofeach arc of said clip by the same percentage.
 4. The clip of claim 3,wherein there is no gap between said fifth arcs and the structure to beattached to said clip.
 5. A method of capturing and turning a fluidabout a structure comprising: attaching a clip to a leading edge of thestructure, wherein the clip has an outside surface, the clip having anose end and a slot end, the slot end including a slot adapted toreceive the structure to be attached to the clip, the clip having twosides between the nose end and the slot end to form the outside surface,each of the two sides starting a midpoint of the nose end and leadingtowards the slot end, the sides together form the outside surface of theclip, each of the sides being composed of five arcs comprising, a firstarc of each side starting at the midpoint of the nose end having aradius of 0.2476 inches and an arc length of 0.22395 inches, a secondarc of each side connected to the first arcs having a radius of 0.5832inches and an arc length of 0.0947 inches, a third arc of each sideconnected to the second arcs having a radius of 0.4636 inches and an arclength of 0.1682 inches, a fourth arc of each side connected to thethird arcs having a radius of 0.3822 inches and an arc length of 0.2263inches, a fifth arc of each side connected to the fourth arcs having anarc having a radius of 0.3291 inches and an arc length of 0.1917 inches,the fifth arc of each side forming the slot end and the slot.
 6. Themethod of claim 5, further including the step of changing size of theclip by scaling by changing arc lengths and arc radius of each arc ofthe clip by the same percentage.
 7. The method of claim 5, furtherincluding the step of placing the structure with the clip in a fluidflow where the flow strikes the clip on one side between the second arcand the fifth arc which causes the flow to warp around the other side ofthe clip.